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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine gives ________ efficiency as compared to an open cycle gas turbine.

None of these
Lower
Same
Higher

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Compressors, Gas Turbines and Jet Engines
The compressor efficiency is the

Compression work/motor input
Isothermal H.P./shaft H.R
Total output/air input
Isothermal H.P/indicated H.R

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Compressors, Gas Turbines and Jet Engines
Efficiency of gas turbine is increased by

Inter cooling
All of the listed here
Reheating
Adding a regenerator

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Compressors, Gas Turbines and Jet Engines
Maximum delivery pressure is a rotary air compressor is of the order of

16 kg/cm²
6 kg/cm²
10 kg/cm²
25 kg/cm²

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Compressors, Gas Turbines and Jet Engines
The pressure ratio of an ideal vaned compressor with increase in mass flow rate

Increases
First decreases and then increases
Remain constant
Decreases

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Compressors, Gas Turbines and Jet Engines
As the turbine inlet temperature increases, the thermal efficiency of gas turbine for the optimum pressure ratio

Decreases
Increases
Remain same
First increases and then decreases

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